[0001] The invention relates to a frangible munition device, more particularly to a common
carrier payload delivery shell, with a frangible safety link.
[0002] There is a requirement to provide munitions that are IM compliant such that they
undergo a low order event in response to a hazard event. There is also a desire that
in the event of a blind, such as where a munition lands without functioning, that
the munition fails in a safe mode.
[0003] According to a first aspect of the invention there is provided a frangible munition
comprising a tail unit, a main body which comprises a payload cavity for receiving
a payload, a fuze, and an explosive train operably connected to said fuze, located
between said main body and the fuze, is a frangible ogive element, wherein the frangible
ogive element and main body are retained in operable engagement by at least one frangible
link, such that upon an impact, said frangible link is caused to fail; such that in
the event of a blind and upon impact with the ground, said frangible link fails so
as to allow venting of any pressure from any energetic events.
[0004] The frangible link may be any connection means, connector or fixing, which operably
links the frangible ogive element to the main body, such that the munition is able
to function in the intended designed mode, but which is severable or shearable upon
application of a substantial force.
[0005] The frangible link may, such as, for example be a shearable thread or at least one
shear pin which retains said main body and frangible ogive element in an operable
engagement.
[0006] The use of a shearble thread allows the frangible ogive element to be reversibly
operably engaged with the main body. The frangible ogive element and main body may
comprise cooperatively engaging male and female threaded portions, wherein at least
one of the threads is a shearable thread. The use of a shearable thread allows the
frangible ogive element to be readily fitted and removed without damaging the shearable
linkage.
[0007] The main body threaded portion may be manufactured from a first material, and the
ogive threaded portion may be manufactured from second material, wherein the second
material has a lower hardness value than the first material, such that upon an applied
force, such as, for example impact with the ground after a blind, the lower hardness
material readily undergoes plastic deformation such that the frangible ogive element
disengages from the main body.
[0008] In a highly preferred arrangement the first material is selected from a steel alloy
and the second material is selected from aluminium or alloy thereof. For gun launched
munitions, such as, for example shells, the forces experienced during launch will
place the shell under uniform compression, however impact with the ground, typically
at an incident angle will place the frangible ogive element and main body under a
tensile load or shearing load, forcing said frangible link to fail, hence allowing
venting of any gaseous outputs. The failure of the frangible link may be substantial
or even cause detachment of the frangible ogive element from the main body. The extent
of the failure is such that if the explosive train or expulsion charge where to function,
after said frangible link has failed that the output may be unconfined i.e. vented,
and reduce the severity of the event. The extent of any energetic material event may
be reduced such that there is a reduced pressure build up and may not cause the primary
payload to be ejected from the shell, or may not cause the primary payload to function.
[0009] The payload may be any commonly used payload such as, for example high explosives,
illumination, smokes, decoys, chaff or a UAV. The payload and payload cavity are selected
such that they are preferably of a uniform dimension, such that any payload may be
readily inserted into the uniform payload cavity of the munition. In a preferred arrangement
the payload is a modular unit. This allows flexibility on logistics, that any payload
may be inserted into any available carrier munition or shell. Conventional smoke and
illumination payloads have bespoke shells or munitions and there is no interchangeability
between munitions.
[0010] In a highly preferred arrangement the frangible ogive element may be used in combination
with a tail unit that is attached to the main body by a further shearable thread.
[0011] The payload may be inserted into the payload cavity from the aft end of the munition.
The payload may be slidably engaged with the payload cavity, such as for example it
may have an engineering fit with payload cavity, such that the payload may be prevented
from moving within a direction which is normal to the elongate axis of the munition.
The payload cavity may have substantially parallel walls, which extend from the intersection
of main body and tail unit up to a locking ring. To prevent movement of the payload
within the cavity along the elongate axis of the munition, the locking ring may be
located between the main body and said frangible ogive element, to retain said payload
within the payload cavity and prevent movement. Preferably the locking ring and main
body comprise cooperatively engaging threaded portions, to allow reversible locking
engagement. This allows the locking ring to compensate for any tolerances in manufacture
of the payload, to ensure that the payload is retained in position.
[0012] The locking ring or the main body of the shell may provide the frangible link with
the frangible ogive element.
[0013] The further shearable thread allows the payload to be reversibly loaded from the
aft of the main body. Prior art shells secure the tail unit to the main body with
shearable pins, which irreversibly fasten the tail unit to the main body, such that
once the munition is constructed the tail unit may only be removed by action of the
device or by applying substantial force, to cause shearing of the pins. The use of
a further shearable thread allows the tail unit to be readily fitted and removed without
damaging the shearable linkage. It is therefore possible to remove the payload for
routine inspection or to fill with a new payload in active theatre.
[0014] In a preferred arrangement the payload is reversibly loadable from the aft end of
the main body. The provision of a threaded tail unit allows the payload to be loaded
and removed from the aft end. In a highly preferred arrangement during use the payload
is capable of being dispensed rearwardly from the main body, upon shearing the further
shearable thread.
[0015] The frangible ogive element is a portion of the munition, typically a shell body,
and may be reversibly operably engaged with the fuze and main body. Preferably the
frangible ogive element, main body and tail unit are secured together by shearable
threads and further shearable threads, respectively.
[0016] The frangible ogive element may have a forward end locatable with said fuze and an
aft end locatable with said main body, wherein the internal diameter of the aft end
of said frangible ogive element may be such that it screws down on the same thread
as that of the locking ring. The locking ring secures the payload within the body
of the shell.
[0017] The fuze may be any known fuze, such as those that respond to selected input or stimuli
or a combination of inputs, such as, for example, mechanical actions of the projectile,
such as the action of high g forces from gun launch or high spin rates from imparted
spin, timed delay, either mechanical or pyrotechnic, caused by separation from the
launch system, or proximity to a target. The fuze may function due to electronic activation,
such as, for example, from an input from a sensor or detector from on-board said munition
or external to the munition. On-board systems may be internal guidance systems. External
stimuli may be provided such as, for example by fly-by wire, remote control, GPS or
target activated laser guidance.
[0018] The fuze may be operably connected to an explosive train, to provide an energetic
output, such as an expulsion charge or detonative output. Where the payload is delivered
during flight i.e. rather than a terminal effect, the payload may be expelled from
the munition by an expulsion charge. In a preferred arrangement said expulsion charge
is suspended in free space within the frangible ogive element, such that it does not
physically contact the payload; this allows for any errors in manufacturing tolerances
between the expulsion charge and the payload. The fuze device may comprise safety
and arming units (SAU), explosive trains to provide sufficient stimuli to the expulsion
charge.
[0019] Where both the frangible ogive element and main body, and the main body and tail
unit are fastened with shearable threaded portions and further shearable threaded
portions, respectively, the further shearable threaded portion has a lower shear strength
than the shearable thread, such that during the intended use of the munition the further
shearable thread between the tail unit and main body fails first, so as to permit
the expulsion of the charge from the aft of the main body.
[0020] According to a further aspect of the invention there is provided a method of dispensing
a payload from a munition as defined herein, comprising the steps of causing initiation
of the expulsion charge, causing shearing of the further shearable thread.
[0021] Whilst the invention has been described above, it extends to any inventive combination
of the features set out above, or in the following description, drawings or claims.
[0022] Exemplary embodiments of the device in accordance with the invention will now be
described with reference to the accompanying drawings in which:-
Figures 1 show an exploded side view of a shell according to the invention.
Figure 2 shows a cross section along the axis of the shell in figure 1.
[0023] Turning to figure 1 there is provided a shell 1, with a main body 5, which is manufactured
from a steel alloy. Located around the circumference of the main body 5 is a copper
driving band 4, which allows engagement with the rifling on the bore of a barrel,
so as to impart spin. A tail unit 2 is located at the aft of the main body 5. The
tail unit 2 is made from aluminium and contains a male threaded portion 3, which engages
with a reciprocal female threaded portion (not shown) located in the aft of the main
body 5. The payload 10 (shown external to the shell 1), when located in the payload
cavity (not shown), inside the main body, is retained in place by use of a locking
ring 6, which screws into the forward end of main body 5. The frangible ogive element
7 has a frangible link 7a, in the form of an aluminium thread. The frangible ogive
element 7 may be secured to the locking ring 6 or directly to the main body 5. The
frangible ogive element receives the expulsion charge 8 and fuze 9. Upon operation
of the fuze 9, the expulsion charge 8 builds up pressure within the frangible ogive
element and at the bursting pressure the thread 3 shears and the payload 10 is expelled
from the aft of the main body 5. During a blind event, the shell 1 would not function
as detailed above, and would hit the ground, wherein the frangible link 7a would be
caused to fail, such that if fuze 9 did erroneously function, that the expulsion charge
8 would be at least partially vented and would not cause the payload 10 to be expelled
from the shell 1.
[0024] Figure 2 shows an illumination shell 20, with a main body 24 formed from a steel
alloy, with a driving band 26 located thereupon. A tail unit 12 is located at the
aft of the main body 24. The tail unit 12 is made from aluminium and contains a male
threaded portion 13, which engages with a reciprocal female threaded portion 14 located
at the aft of the main body 24.
[0025] The payload 22 is located in the payload cavity 15, and is retained in place by use
of a locking ring 16, which screws into the forward end of main body 24. The payload
22 is a modular illumination or smoke payload, (contents not shown) which slides into
the payload cavity 15.
[0026] The frangible ogive element 17 has a frangible link 17a, in the form of an aluminium
thread, which is fastened to the locking ring 16. The frangible ogive element receives
the expulsion charge 18 and fuze 19. Upon operation of the fuze 19, the expulsion
charge 18 builds up pressure within the frangible ogive element and at the bursting
pressure the thread 13 shears and the payload 22 is expelled from the aft of the main
body 24.
[0027] Upon operation of the fuze 19, the expulsion charge 18 builds up pressure within
the frangible ogive element 17 and at the bursting pressure the thread 13 shears and
the payload 22 is expelled from the aft of the main body 24.
[0028] During a blind event, the fuze 19 would not function as detailed above, and the shell
20 would hit the ground, wherein the frangible link 17a would be caused to fail. Therefore
if the fuze 19 did erroneously function, the expulsion charge 18 would be at least
partially vented via the failed frangible link and would not cause the payload 22
to be expelled from the shell 20.
1. A frangible munition comprising a tail unit, a main body which comprises a payload
cavity for receiving a payload, a fuze, and an explosive train operably connected
to said fuze, located between said main body and the fuze, is a frangible ogive element,
wherein the frangible ogive element and main body are retained in operable engagement
by at least one frangible link, such that upon an impact, said frangible link is caused
to fail.
2. A munition according to claim 1, wherein the frangible link is a shearable thread
or at least one shear pin.
3. A munition according to claim 2, wherein the main body comprises a first threaded
portion manufactured from a first material, and the frangible ogive element comprises
a second threaded portion manufactured from second material, wherein the second material
has a lower hardness value than the first material.
4. A munition according to claim 3, wherein the first material is selected from a steel
alloy and the second material is selected from aluminium or alloy thereof.
5. A munition according to any one of the preceding claims, wherein there is a locking
ring located between the main body and said frangible ogive element, to retain said
payload within the payload cavity.
6. A munition according to claim 4, wherein the locking ring and main body comprise cooperatively
engaging threaded portions.
7. A munition according to any one of the preceding claims, wherein the frangible ogive
element has a forward end locatable with said fuze and an aft end locatable with said
main body, wherein the internal diameter of the aft end of said frangible ogive element
is substantially the same as the internal diameter of said payload cavity.
8. A munition according to any one of the preceding claims wherein the fuze is operably
connected to at least one expulsion charge, wherein said charge is suspended in free
space.
9. A munition according to any one of the preceding claims wherein the payload cavity
has substantially parallel walls, which extend from the intersection of the tail unit
to the locking ring.
10. A munition according to any one of the preceding claims wherein the payload is a modular
unit.
11. A munition according to claim 10, wherein the modular unit, is reversibly loadable
from the aft end of the main body.
12. A munition according to any one of the preceding claims wherein the payload is capable
of being dispensed rearwardly from the main body, upon shearing the shearable thread.
13. A method of dispensing a payload from a munition according to any one of the preceding
claims, comprising the steps of causing initiation of the expulsion charge, causing
shearing of the shearable thread.
14. A device substantially as described herein with reference to the accompanying drawings.